Powder Corrosion and Chip-Resistant Coating

ABSTRACT

A powder composition including a resin and from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment, optionally including from 0% to 65%, by weight based on powder composition weight, zinc, the composition being substantially free from pigment providing a metallic effect is provided. The corrosion-inhibiting pigment may be present in amounts of up to 50%, by weight based on powder composition weight, for example, up to 35%. A method for coating a substrate with the powder composition and the coated substrate so formed are also provided.

This application claims the benefit of priority under 35 U.S.C. §119(e) of U.S. Provisional Patent Application No. 61/211, 847 filed on Apr. 3, 2009.

This invention relates to a powder composition suitable for powder coating. More particularly this invention relates to a powder composition including a resin and from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment, the composition being substantially free from pigment providing a metallic effect. This invention also relates to a method for coating a substrate with the powder composition and a coated substrate.

U.S. Pat. No. 7,244,780 discloses powder coating compositions that comprise a film-forming polymer, a pigment such as aluminum flake providing a metallic effect and a stabilizing additive that inhibits degradation of the metallic pigment.

U.S. Pat. No. 7,018,716 discloses corrosion-and chip-resistant coatings for high tensile steel components, such as automotive coil springs, formed from a coating powder composition of “toughened” epoxy resin. In a single coat embodiment, the entire coating is loaded with at least 75 phr zinc powder. In a dual coat embodiment, an inner coat is loaded with at least 75 phr zinc and an outer, zinc-free coating is reinforced by the addition of fibers and/or by a foaming agent which renders it porous.

There has been a need for a powder composition suitable for coating a substrate, particularly a steel substrate such as, for example, high tensile steel wherein a coating formed from the composition exhibits a high level of chip resistance and corrosion resistance without relying on the use of high levels of zinc metal. The powder composition of the present invention is capable of exhibiting a high level of chip resistance and corrosion resistance without relying on the use of high levels of zinc metal.

In a first aspect of the present invention, there is provided a powder composition comprising a resin and from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment, said composition being substantially free from pigment providing a metallic effect. The corrosion-inhibiting pigment may be present in amounts of up to 50%, by weight based on powder composition weight, or up to 40%,or up to 35%.

In a second aspect of the present invention there is provided a method for coating a substrate comprising: forming a powder composition comprising a resin and from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment, said composition being substantially free from pigment providing a metallic effect; applying said powder composition to a substrate; and heating said powder composition to fuse and cure said applied composition. The corrosion-inhibiting pigment may be used in amounts of up to 50%, by weight based on powder composition weight, or up to 40%,or up to 35%.

In a third aspect of the present invention there is provided a method for coating a substrate comprising: forming a first powder composition comprising a resin and from 0% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment, said first powder composition being substantially free from pigment providing a metallic effect; applying said first powder composition to said substrate; forming a second powder composition comprising a resin and from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment, said composition being substantially free from pigment providing a metallic effect; applying said second powder composition to said substrate coated with said first powder composition; and heating said applied powder compositions to fuse and cure said compositions. In each of the first and second powder compositions, the corrosion-inhibiting pigment may be present in amounts of up to 50%, by weight based on powder composition weight, or up to 40%,or up to 35%.

In a fourth aspect of the present invention there is provided a coated substrate comprising said substrate bearing a coating comprising a resin and from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment. The coating may comprise corrosion-inhibiting pigment in amounts of up to 50%, by weight based on powder composition weight, or up to 40%, or up to 35%.

The powder composition of the present invention includes at least one resin, i.e., a polymeric composition suitable for powder coatings such as, for example, thermoplastic or thermoset resins, particularly an epoxy resin. The epoxy resin may be chosen from a variety of epoxy resins useful for coating powders known in the art, such as those produced by the reaction of epichlorohydrin or polyglycidyl ether and an aromatic polyol such as bisphenol, e.g., bisphenol A. The epoxy resin typically has an epoxy functionality greater than 1.0 and more preferably greater than 1.9. Generally the epoxy equivalent weight should be at least 170, but lower values may be acceptable in some cases. Preferably the epoxy equivalent weight is less than 2300, and more preferably from 800 to 1500. Such epoxy resins may be produced, for example, by an etherificiation reaction between an aromatic or aliphatic polyol and epichlorohydrin or dichlorohydrin in the presence of an alkali such as caustic soda. The aromatic polyol may be, for example, bis(4-hydroxyphenyl)-2,2-propane (i. e. bisphenol A), bis(4-hydroxyphenyI)-1,1-ethane, bis(4-hydroxyphenyl)-1, 1-isobutane, bis(4-hydroxy-t-butylphenyl)-2,2-propane, bis(2-hydroxynaphthyl)methane, 4,4′-dihdyroxybenzophenone or 1,5-pentanediol, 1, 6-hexanediol, diethylene glycol, triethylene glycol, polyethylene glycol, polypropylene glycol or dipropylene glycol, for example diglycidyl ethers or condensed glycidyl ethers of such diols, can be used. Other oxirane group-containing polymers that can be used as the epoxy resin in hybrid powder coating compositions according to this invention include polyglycidyl-functional acrylic polymers or epoxy novolak resins. Preferred epoxy resins for use in the present invention are those based on bisphenol A.

The powder composition may further incorporate one or more of toughening, foaming, and reinforcing technologies. “Toughening technology” herein refers to modification of the resin component to provide a tougher applied coating. “Foaming technology” herein refers to powder compositions selected to engender foam structure in the applied coating. “Reinforcing technology” herein refers to additional components in the powder composition selected to reinforce the applied coating.

Epoxy resin may be toughened by the use of additives or co-reactants such as, for example, as impact modifiers, flexibilizing agents, plasticizers and tougheners. These may include:

elastomeric modifications, either within the base polymer, reacted into the coating composition through cross-linking, or as unreacted additives, such as, for example, CTBN rubber, butadiene/styrene, nitrile, neoprene, acrylic, butyl, ethylene/propylene/diene, polysulfide, polyisoprene, silicone, and urethane rubber;

random or block copolymer addition which offer some degree of internal plastication and may be exemplified by the FORTEGA™ products (Dow Chemical Co.);

addition of plasticizers such as epoxidized soybean oil;

crosslinked or noncrosslinked core/shell resins with various compositions such as epoxy, acrylic, polyurethane representing either the core or the shell portion.

Further, tougheners may include hollow spherical particle including polymeric or glass beads.

Discrete microdomains of any of the above may be present and may contribute to chip resistance.

In one embodiment the epoxy resin, preferably a bisphenol A resin, is adducted to an elastomer having a T_(g) of −30° C. or below, preferably −40° C. or below. The preferred elastomer is CTBN rubber. Such epoxy/CTBN rubber adducts are described, for example, in U.K. Patent Specification 1,407,851 (C. G. Taylor) published Sep. 24, 1975 and Powder Coatings, 184 “Elastomer-Modified Epoxy Powder Coatings: a Review”, Apr. 13, 1994, No. 4347. To provide the toughening (flexibilizing) for cold-temperature chip resistance, the CTBN component should be present at least 5 wt % of the total of the CTBN and the epoxy components. Above about 25 wt % CTBN, no further benefit is realized and it is not desired to exceed 25 wt % lest there be insufficient epoxy component for a good cure. The fact that the elastomer component is chemically bound to the epoxy component, i.e., by esterification reaction of the carboxyl groups of the CTBN with epoxy groups, ensures that a complete phase separation does not occur during fusion and curing of the coating powder. However, there are microdomains of epoxy and rubber.

In an alternative embodiment, a core/shell resin is used in which an acrylic rubber resin forms the core and the epoxy resin, preferably a bisphenol A epoxy resin, forms the shell. Again, chemical bonding between carboxylic functionality of the acrylic rubber resin of the core and the epoxy resin of the shell prevents phase separation during fusion and curing of the coating powder formed using the core/shell resin. Such acrylic rubber modified epoxies are described, for example, in Polymer Reprints, 32(3), pp. 358-9 by H-J Sue and E. I. Garcia-Melfin.

In another embodiment thermosetting epoxy resins may include either a cross-linking agent, such as a polyhydroxyl compound or a cure catalyst to effect auto-cross-linking of the epoxy resin. For example, the epoxy resin is cured with a polyhydroxyl functionality having a relatively high hydroxy equivalent weight, i.e., at least about 200 up to about 500, preferably at least about 300. The relatively high hydroxy equivalent weight of the cross-linking agent ensures relatively long chain length between OH groups, which chain lengths provide flexibility to the cured coating, helping to render the coatings chip-resistant. Suitable curing agents useful in the practice of this invention are exemplified by phenolic curing agents, such as a bisphenol A end capped diglycidyl ether of bisphenol A, which is the reaction product of a diglycidyl ether of bisphenol A and bisphenol A and polyester resins with free carboxylic acid groups that are known to form “Hybrid” powder coatings. Examples of preferred phenolic curing agents for the epoxy resin component include those sold under the trademarks D.E.H.™87 and D.E.H.™85 (Dow Chemical Co.), both of which are believed to be bisphenol A end capped diglycidyl ethers of bisphenol A. Other classes of phenolic hardeners can be used as well such as phenol-and cresol-novolac curing agents sold by Dow Chemical Co. Hexion Specialty Chemicals.

Other epoxy crosslinking agents include, for example:

amines, including multifunctional aliphatic or aromatic primary or secondary amines, such as dicyandiamide, diaminodiphenyl sulfone;

tertiary amines which promote self cross-linking such as DMP 30 (Dow Chemical Co.).;

boron trihalides and salts thereof such as the monoethanolamine salt of boron trifluoride.;

Organic acid salts such as VESTAGON™B55 and VESTAGON™B68 (Degussa Corp.).;

di and poly anhydrides such as benzophenonetetracarboxylic dianhydride (BTDA);

di and poly phenols such as methylene disalicylic acid; and,

di imidazoles, substituted imidazoles and epoxy imidazole adducts such as 2-methyl imidazole or DEH 40 (Dow Chemical Co.).

The powder composition of the present invention is a resin-based composition that includes from 5% to 70%, by weight based on powder composition weight, of a corrosion-inhibiting pigment. The corrosion-inhibiting pigment may be, for example, at least one of:

simple molybdates such as zinc molybdate, strontium molybdate and complex molybdates such as calcium zinc molybdate, calcium zinc phosphomolybdate (eg., MOLYWHITE™ MZAP);

simple chromates such as zinc chromate, barium chromate, strontium chromate, magnesium chromate, calcium chromate and complex chromates such as lead silico chromate, zinc tetraoxy chromate;

metal phosphides such as iron phosphide (e.g. FERROPHOS™ iron phosphide, OCCIDENTAL CHEMICAL CORP., Dallas, Tex.);

silicates such as zinc phosphosilicate and calcium borosilicate; and

simple phosphates such as iron phosphate, zinc phosphate, zinc pyrophosphate, calcium hydrogen phosphate and complex phosphates such as zinc borate orthophosphate, strontium aluminum polyphosphate, zinc aluminum polyphosphate, zinc aluminum molybdenum orthophosphate, zinc aluminum orthophosphate.

The pigments may be present in their basic form, may be organic modified, and may be present as the hydrate. Other descriptions of suitable corrosion-inhibiting pigments appear in U.S. Pat. No. 3,884,705 and are summarized by G. B. Rothenberg in Paint Additives, Noyes Data Corp, 1978, pp175-177. U.S. Pat. No. 7,244,780 also discloses corrosion-inhibiting pigments that include “a source of stabilizing anions, advantageously phosphate ions, capable of dissolving in the presence of water”.

Zinc phosphate herein is contemplated to include (a) Zinc phosphate di-or tetra-hydrate, preferably in the form of spheroidal particles as described in U.S. Pat. No. 5,137,567 (an example of zinc phosphate dihydrate being the material available under the trade name DELAPHOS™ 2M and a further example of a zinc phosphate being the available under the trade name HISPAFOS™ SP, comprising spheric particles of narrow particle size distribution); (b) Spheroidal zinc phosphate as a crystalline phase in admixture with an amorphous phase comprising Fe(II) phosphate and Fe(III) phosphate. Further information concerning such materials may be found in U.S. Pat. No. 5,030,285; and (c) Zinc phosphate (preferably in spheroidal form) modified with zinc molybdate (such as ACTIROX™106; Microfine Minerals Ltd.)

The powder composition optionally includes from 0% to 65%, by weight based on powder composition weight, zinc; typically the zinc is in powder or flake form. Preferably the powder composition includes a minimal amount of zinc; more preferably the powder composition is free from zinc.

The powder composition of the present invention is “substantially free from pigment providing a metallic effect”, which means that the total proportion of metallic pigment(s) incorporated in the powder coating composition shall be less than 0.1% by weight (based on the weight of the composition without the metallic pigment(s)); preferably no metallic pigment is included in the powder composition. By “a pigment providing a metallic effect” herein is meant a metallic pigment typically in flake form such as, for example, aluminium or an aluminium alloy or another metal or alloy, for example, stainless steel, copper, tin, bronze or brass typically used to produce various metallic effects including those referred to as “metallic”, “effect”, “lustre”, or “glamour” finishes.

The metallic pigment may be an uncoated or coated material. Examples of coated materials include pigments coated with silica or another inert inorganic material for greater chemical resistance and durability. Alternatively, the pigment may be coated with a plastics material for similar purposes, for example, an acrylic, PTFE or thermosetting plastics material, or may be provided in a polymer or plasticizer which is compatible with the film-forming binder of the powder coating composition. As a further possibility, the metallic pigment may be coated with a coloring agent such as a metal oxide pigment such as, for example, iron oxide, to provide special color effects.

Powder compositions used to provide the chip-resistant and corrosion-resistant coatings of the present invention are produced in the usual manner. The components are blended, and then are melt-compounded with heating above the melting point of the resin for a short time, e.g., 30 to 90 sec., so that no significant curing occurs. The molten compound is extruded, and after extrusion, the composition is rapidly cooled. The composition is then ground and, as necessary, the particulates sorted according to size. For electrostatic coating, the particles are generally in the 5 to 100 micron size range with a major portion generally being in the 20 to 40 micron size range. Larger particulates are useful for fluidized bed coating operations.

In the method for coating a substrate of the present invention the powder composition of the present invention is applied to the substrate and heated to fuse and cure the applied composition. In one embodiment the substrate is a metal substrate, typically a steel substrate, wherein the powder composition may be may be used, for example, as a pipe coating, rebar coating, or a coating for agricultural or construction equipment. In another embodiment the substrate is a high tensile steel substrate such as is suitable for use, for example, in coil springs in the transportation industry. Herein, high tensile steel is defined as having MPa (megapascal (N/m ²) ranging from 1800 Mpa to 2100 Mpa or above; this includes super high tensile steel from 1950 Mpa to 2100 Mpa or above. Steel substrates herein are contemplated to include pretreated steel substrates, including treatments of, for example, zinc phosphate, iron phosphate, and dry in place pretreatment technology. The powder composition is typically heated at a temperature of greater than 149° C. (300° F.) for a time sufficient to fuse and substantially cure the coating such as, for example, by placing into an electric air circulating oven maintained at 160° C (320° F.) for 20 minutes for a cured film thickness of 50 to 101 μm (2.0-4.0 mils). It is understood that thermoplastic resins do not include a cure mechanism and therefore will only fuse under heating.

In the method for coating a substrate of the present invention the powder composition may be applied as a single coat, with sufficient film thickness for chip resistance protection. In an alternative embodiment the powder composition may be applied as a single foamed coat, the foam having been engendered by the use of a separate foaming agent or by the temperature-dependent inherent foaming of certain phosphate and related constituents such as, for example, zinc phosphate. Optionally, the powder composition may incorporate reinforcing technology, that is, the composition may include carbon fibers, slip agents, barium sulfate, calcium carbonate, wollastonite, or any materials that will reinforce the coating to enhance chip resistance.

In an alternative method of the present invention a two coat method may be employed. In such embodiments a first coat (base coat) is applied and the basecoat may be partially or fully cured. Then a subsequent second coat (top coat) is applied to the base coat and the coats are fused and cured. Either of the first coat, the second coat, or both first and second coats, independently, is formed from the powder composition of the present invention. Either of the first coat, the second coat, or both first and second coats may independently be foamed coats as described hereinabove. Either of the first coat, the second coat, or both first and second coats may independently include carbon fibers, slip agents, barium sulfate, calcium carbonate, wollastonite, or any materials that will reinforce the coating to enhance chip resistance.

The introduction of cellular foam structures is not limited to the organic portion of the protective system. For example, the steel cleaning and “pretreatment ” or passivation step may introduce and or include foam forming components which generate a cellular structure within the pretreatment layer or the organic layer above it as evolved gases percolate through the film during heating. Examples of such gas generators are azo compounds, well known in the industry. Such foam may also be produced by simple decomposition or dehydration of the pretreatment chemicals themselves. Zinc phosphate (hopeite and/or phosphyllite), for example, having been deposited on cold rolled steel panels, has been shown to foam by heating to approximately 200° C.

The coated substrate of the present invention bears a coating including a resin and from 5% to 70%, by weight, based on powder composition weight, of a corrosion-inhibiting pigment, optionally further including from 0% to 65%, by weight based on powder composition weight, zinc, the composition being substantially free from pigment providing a metallic effect. It is formed by the above-described method of the present invention.

EXAMPLE 1 Formation of Powder Compositions and Application to Substrates

TABLE 1.1A Powder compositions Zinc Phosphate-Containing Base Coat compositions Example No. 1-1 1-2 1-3 1-4 2-1    5%   10%   20%   30%   44% Zn3(PO4)2 Zn3(PO4)2 Zn3(PO4)2 Zn3(PO4)2 Zn3(PO4)2 Epoxy resin A 92 92 92 92 92 Imidazole 3 3 3 3 3 adduct B Carbon black 3 3 3 3 3 pigment Hydroxy 20.8 20.8 20.8 20.8 20.8 compound C Epoxy resin D 8 8 8 8 8 Zinc Dust 0 0 0 0 0 Zinc Phosphate 6.7 14.5 32 54 100 Fumed silica 0.30% 0.30% 0.30% 0.30% 0.30% Other Corrosion-Inhibiting Base Coat compositions 3-1 3-2 3-3 3-4 3-5 Epoxy resin A¹ 92 92 92 92 92 Imidazole adduct 3 3 3 3 3 B² Carbon black 3 3 3 3 3 pigment Hydroxy 20.8 20.8 20.8 20.8 20.8 compound C³ Epoxy resin D⁴ 8 8 8 8 8 Zinc Dust 237.5 225 200 175 150 Zinc Phosphate 0 0 0 0 0 FERROPHOS ™ 12.5 25 50 75 100 Strontium Zinc 0 0 0 0 0 Phosphosilicate Calcium 0 0 0 0 0 Borosilicate Fumed Silica 0.30% 0.30% 0.30% 0.30% 0.30% ¹Diglycidyl ether of bisphenol A epoxy resin with a weight per epoxide between 935 and 1175. ²Imidazole adduct with a diglycidyl ether of bisphenol A epoxy resin. ³Bisphenol A end capped diglycidyl ether of bisphenol A with a hydroxyl equivalent weight between 370 and 400. ⁴Master Batch epoxy resin containing 90 wt % of a diglycidyl ether of bisphenol A epoxy resin with a weight per epoxide between 795 and 895 and 10 wt % of acrylic flow modifier.

TABLE 1.1B Powder compositions Zinc Phosphate-Containing Base Coat compositions Example No. 2-2 44% Zn3(PO4)2 2-3 2-4 2-5 2-6 Control Epoxy 92 92 92 92 92 92 resin A Imidazole 3 3 3 3 3 3 adduct B Carbon 3 3 3 3 3 3 black pigment Hydroxy 20.8 20.8 20.8 20.8 20.8 20.8 compound C Epoxy 8 8 8 8 8 8 resin D Zinc Dust 150 175 200 225 237 250 Zinc 100 75 50 25 12.5 0 Phosphate Fumed 0.30% 0.30% 0.30% 0.30% 0.30% 0.30% silica Other Corrosion-Inhibiting Base Coat compositions 4-1 4-2 4-3 4-4 Epoxy resin A¹ 92 92 92 92 Imidazole adduct B² 3 3 3 3 Carbon black 3 3 3 3 pigment Hydroxy 20.8 20.8 20.8 20.8 compound C³ Epoxy resin D⁴ 8 8 8 8 Zinc Dust 0 0 0 0 Zinc Phosphate 0 0 0 0 FERROPHOS ™ 0 0 0 0 Strontium Zinc 3.2 14 0 0 Phosphosilicate Calcium Borosilicate 0 0 6.7 22.4 Fumed Silica 0.30% 0.30% 0.30% 0.30% ¹Diglycidyl ether of bisphenol A epoxy resin with a weight per epoxide between 935 and 1175. ²Imidazole adduct with a diglycidyl ether of bisphenol A epoxy resin. ³Bisphenol A end capped diglycidyl ether of bisphenol A with a hydroxyl equivalent weight between 370 and 400. ⁴Master Batch epoxy resin containing 90 wt % of a diglycidyl ether of bisphenol A epoxy resin with a weight per epoxide between 795 and 895 and 10 wt % of acrylic flow modifier.

Powder samples were electrostatically applied onto 7.68cm×12.8cm×0.082 cm (3 inch×5 inch×0.032 inch) steel panels. Panels were supplied by ACT Laboratories, Inc., B-958, P-60 (Zinc Phosphate/Non Chrome Rinse). Powder coated panels were placed into an electric air circulating oven maintained at 160° C. (320° F.) for 20 minutes. Cured film thickness was 50 to 101 μm (2.0-4.0 mils).

EXAMPLE 2 Evaluation of Powder Coated Panels

Each of the coated panels exhibited a direct/reverse impact rating of 1.84 kg-m (160 in-lb)/1.84 kg-m (160 in-lb).

The coated panels of Example 1 were scribed with an ‘X’ and placed in a Salt Fog Cabinet According to ASTM Method B 117. At intervals panels were removed from the cabinet and scraped with a dull knife, perpendicularly to scribed lines. Maximum undercutting (corrosion) was measured in inches outwardly from the scribe line. Panels were typically exposed for 3000 to 4000 hours.

As shown in Table 2.1, below, the powder composition-coated panels of the present invention, Examples 1-1, 1-2, 1-3, 1-4, and 2-1, exhibited a useful level of impact resistance and salt spray corrosion resistance.

TABLE 2.1 Creepback from X-scribe during ASTM B 117 Salt Spray Exposure Example No. Comparative 1-1 1-2 1-3 1-4 2-1 HOURS 66% Zn 5% 10% 20% 30% 44% EXPOSED Dust Zn3(PO4)2 Zn3(PO4)2 Zn3(PO4)2 Zn3(PO4)2 Zn3(PO4)2 192 NC NC NC NC NC NC 384 NC NC NC NC NC NC 552 NC NC NC NC NC NC 672 NC NC NC NC NC NC 840 NC NC NC NC NC NC 1008 NC <1/32″ <1/32″ <1/32″ <1/32′ <1/32″ 1176 NC NC <1/32″ <1/32″ <1/32′ NC 1344 NC <1/32″ <1/32″ <1/32″ <1/32′ <1/32″ 1512 NC <1/32″ <1/32″ <1/32″ <1/32′ <1/32″ 1680 <1/32″ <1/32″ <1/32″ <1/32″ <1/32′ <1/32″ 1848 <1/32″ <1/32″ 1/32″ 1/32″ <1/32′ <1/32″ 2016 <1/32″ 1/32″ 1/32″ 1/32″ 1/32″ 1/32″ 2184 <1/32″ 1/32″ 1/32″ 1/32″ <1/32″ <1/32″ 2352 <1/32″ 1/32″ 1/32″ 1/32″ 1/32′ <1/32″ 2520 <1/32″ >1/32″ 1/16″ 1/32″ >1/32″ <1/32″ 2688 <1/32″ 1/16″ 1/16″ 1/16″ 1/16′ 1/32″ 2856 <1/32″ 1/16″ >1/16″ 1/16″ 1/16′ 1/16″ 3024 <1/32″ 1/16″ 3/32″ 3/32″ 3/32″ 1/16″ 3192 <1/32″ 1/16″ 3/32″ 3/32″ 3/32″ 1/16″ 3360 1/32″ 3/32″ ⅛″ >3/32″ 3/32″ 1/16″ 3528 1/32″ 3/32″ ⅛″ ⅛″ 3/32″ 1/16″ 3696 1/32″ 3/32″ ⅛″ ⅛″ 3/32″ 1/16″ 3864 1/32″ ⅛″ 3/16″ ⅛″ ⅛″ 1/16″ 4056 1/16″ ⅛″ >1/4″ 3/16″ 3/16″ 3/32″ 

1. A method of coating a high tensile steel substrate with a chip and corrosion resistant coating, the method comprising (a) applying to the substrate a powder composition comprising (i) an epoxy resin based on bisphenol A, (ii) a polyhydroxyl functional phenolic curing agent having a HEW of about 200 to about 500, and (iii) from 5% to 70% by weight based on powder composition weight of a corrosion-inhibiting pigment selected from the group consisting of molybdates, chromates, metal phosphides, silicates and phosphates, wherein the composition comprises zinc in an amount of 0% to 65% by weight based on the powder composition; and (b) heating the applied powder composition to fuse and cure the composition.
 2. The method according to claim 1 wherein the powder composition further comprises at least one additive that toughens the powder composition, aids in foaming the powder composition, or reinforces the powder composition.
 3. The method according to claim 1 wherein the epoxy resin is a thermoplastic resin or a thermoset resin.
 4. The method according to claim 1 wherein the epoxy resin has an epoxy equivalent weight of less than
 2300. 5. The method according to claim 1 wherein the epoxy resin is adducted to an elastomer.
 6. The method according to claim 1 wherein the corrosion-inhibiting pigment is selected from the group consisting of simple molybdates, complex molybdates, simple chromates, complex chromates, metal phosphides, silicates, simple phosphates and complex phosphates.
 7. The method according to claim 1 wherein said powder composition is substantially free from pigment providing a metallic effect.
 8. The method according to claim 2 wherein the at least one additive is an additive that toughens the powder composition, wherein the additive is selected from the group consisting of elastomeric modifications, a random or block copolymer addition, addition of plasticizers, crosslinked or non-crosslinked core/shell resins, hollow spherical particles and discrete micro-domains thereof.
 9. The method according to claim 8 wherein the additive is a random or block copolymer addition.
 10. The method according to claim 1 wherein the at least one corrosion-inhibiting pigment is selected from the group consisting of zinc phosphate, strontium zinc phosphosilicate, calcium borosilicate, iron phosphide, strontium chromate, zinc molybdate and mixtures thereof. 